North American B-25 'Mitchell'The North American B-25 Mitchell was an American twin-engined medium bomber manufactured by North American Aviation. It was used by many Allied air forces, in every theater of World War II, as well as many other air forces after the war ended, and saw service across four decades. Development The North American B-25 'Mitchell' was an American twin-engined medium bomber manufactured by North American Aviation originally designated NA-40B a twin-engined five seat bomber to meet 1938 USAAF requirement for attack bomber. Powered by two 1,100 hp (825 kW) Pratt & Whitney R-1830-56C3G radials. It required 8,500 original drawings and 195,000 engineering man-hours to produce the first one. The prototype NA-40 was first flown in January 1939 by Paul Balfour. The modified and improved NA-40B was submitted to the United States Army Air Corps for evaluation. A product of Dutch Kindelberger's North American team was to be an efficient, easy to manufacture and repair and was able to do any job assigned to it. The B-25 was named in honor of General Billy Mitchell, a pioneer of U.S. military aviation. When the production version of the B-25 first flew on August 19, 1940, the airplane had been given additional power in the form of its Wright GR-2600 engines. The initial B-25 was lacking in directional stability, and examples after number ten had the wings "gulled" to reduce the amount of dihedral (the angle between the wing and an intersecting horizontal). An improvement of the NA-40B, dubbed the NA-62, was the basis for the first actual B-25. This aircraft was originally intended to be an attack bomber for export to the United Kingdom and France, both of which had a pressing requirement for such aircraft in the early stages of World War II. However, those countries changed their minds, opting instead for the Douglas DB-7. Back to TopInto Service The Pacific and Far East The majority of B-25s in American service were used in the Pacific. It fought on Papua New Guinea, in Burma and in the island hopping campaign in the central Pacific. It was in the Pacific that the aircraft's potential as a ground attack aircraft was discovered and developed. The jungle environment reduced the usefulness of standard-level bombing, and made low-level attack the best tactic. The ever-increasing amount of forward firing guns was a response to this operational environment, making the B-25 a formidable strafing aircraft. Fighting the Luftwaffe The first B-25s arrived in Egypt just in time to take part in the Battle of El Alamein in November 1942. From there the aircraft took part in the rest of the campaign in North Africa, the invasion of Sicily and the advance up Italy. In Italy the B-25 was used in the ground attack role, concentrating on attacks against road and rail links in Italy, Austria and the Balkans. The five bombardment groups that used the B-25 in the desert and Italy were the only U.S. units to use the B-25 in Europe. Back to TopOther Nations The Royal Air Force (RAF) was an early customer for the B-25 via Lend-Lease. The RAF was the only force to use the B-25 on raids against Europe from bases in the United Kingdom. A total of 93 Mitchell Is and IIs had been delivered to the RAF by the end of 1942 and served with No. 2 Group RAF, the RAF's tactical medium bomber force. The first RAF operation with the Mitchell II took place on 22 January 1943, when six aircraft from No. 180 Squadron RAF attacked oil installations at Ghent. After the invasion of Europe, all four Mitchell squadrons moved to bases in France and Belgium (Melsbroek) to support Allied ground forces. The British Mitchell squadrons were joined by No. 342 (Lorraine) Squadron of the French Air Force in April 1945.
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Specifications(B-25J):
Country of Origin: USA Crew: 6 Length: 52 ft 11 in (16.13 m) Wingspan: 67 ft 7 in (20.60 m) Height: 16 ft 4 in (4.98 m) Empty weight: 19,480 lb (8,855 kg) Max. takeoff weight: 35,000 lb (15,910 kg) Powerplant: 2 × Wright R-2600-92 14-cylinder air-cooled radial engine, 1,700 hp (1,267 kW) each Performance Maximum speed: 272 mph (237 kn, 438 km/h) at 13,000 ft (3,960 m) Cruise speed: 230 mph (200 knots, 370 km/h) Range: 1,350 mi (1,174 nmi, 2,174 km) Service ceiling: 24,200 ft (7,378 m) Armament Guns: 12 18 × .50 in (12.7 mm) M2 Browning machine guns in top turret, nose, tail and two waist positions Bombs: Hardpoints: 2,000 lb (900 kg) ventral shackles to hold one external Mark 13 torpedo Rockets: racks for eight 5 in (127 mm) high velocity aircraft rockets (HVAR) Bombs: 3,000 lb (1,360 kg) bombs |